Composite structures

ABSTRACT

In accordance with at least one aspect of this disclosure, a composite structure can be formed of or including a plurality of composite strips. The plurality of composite strips include one or more filler strips which can have at least one filler edge having a filler edge geometry between a first surface and second surface, the second surface being opposite the first surface. The filler edge geometry can be configured to prevent formation of one or more gaps between one or more adjacent composite strips.

FIELD

This disclosure relates to composite structures.

BACKGROUND

There are risks of damage initiation in certain composite structures(e.g., composite drive shafts) in areas of non-uniform thickness, forexample, in the vicinity of ends of individual plies. Such areas areusually designed to create tapered shapes, e.g., in case of compositedrive shafts, in zones of joints (to add extra thickness to compensatelocal stress concentrations due to metallic fasteners) or rub-rings (toadd extra thickness to mitigate potential contacts), for example.

Such conventional designs and corresponding manufacturing methods andsystems have generally been considered satisfactory for their intendedpurpose. However, there is still a need in the art for improved damagetolerance of composite structures. The present disclosure provides asolution for this need.

SUMMARY

In accordance with at least one aspect of this disclosure, a compositestructure can be formed of or can include a plurality of compositestrips. In embodiments, the plurality of composite strips can include afiber-reinforced polymer-matrix. The plurality of composite strips caninclude one or more filler strips which can have at least one filleredge having a filler edge geometry between a first surface and secondsurface, the second surface being opposite the first surface. The filleredge geometry can be configured to prevent formation of one or more gapsbetween one or more adjacent composite strips.

The filler edge geometry can be non-straight (e.g., a non-flat, non-90degree face) between the first surface and the second surface of the oneor more composite strips. For example, the filler edge geometry can havea chamfer between the first surface and the second surface.

In certain embodiments, the at least one filler edge is a transverse endof the one or more composite strips. The one or more compositestructures can include a plurality of layers sandwiching the transverseend. The transverse end can be located at a transition position wherethere is a change in a total amount of layers.

In certain embodiments, the filler edge geometry can be a double beveledshape having a first straight slope from the first surface to a tip, anda second straight slope from the second surface to the tip. In certainembodiments, the first straight slope and the second straight slope canhave different lengths and/or slopes.

The filler edge geometry can include a curved shape having at least afirst curved slope from the first surface to a tip and/or the secondsurface. In certain embodiments, the first curved slope can be convex.In certain embodiments, the first curved slope can be concave.

The curved shape can include a second curved slope from the secondsurface to the tip. The first curved slope and/or the second curvedslope can be convex or concave, or a combination thereof (e.g., thefirst curved slope and the second curved slope can be the same ordifferent).

In certain embodiments, the composite structure can form a beam orhollow shaft having changing layer amounts at one or more ends thereofsuch that the one or more ends have more total layers. In certainembodiments, the one or more composite strips form terminal layers atthe one or more ends that do not extend the entire length, wherein thefiller edges are located at the one or more ends of the terminallayer(s), where one or more longer layers would bend (e.g., where aresin gap would have existed otherwise). In certain embodiments, thecomposite strips can form a curved structure. The filler edges can belocated at the one or more ends of the terminal layers, where one ormore longer layers bend. Any other suitable composite structure shapes,layer arrangements, and/or purpose are contemplated herein.

In accordance with at least one aspect of this disclosure, a method caninclude laying a composite strip to form a composite structure, andcutting or otherwise forming at least one transverse end of thecomposite strip to have a filler edge having a filler edge geometrybetween a first surface and second surface, the second surface beingopposite the first surface, the filler edge geometry configured toprevent formation of one or more gaps between one or more adjacentcomposite strips. In certain embodiments, cutting or otherwise formingcan include cutting the end of the composite strip at a non-90 degreeangle, with respect to a reinforced fiber orientation.

Cutting the end can include making a single cut to form a chamfer, or adouble cut to form a double bevel with a tip. Cutting or otherwiseforming can include clamping the end of the composite strip into a form.The method can include any other suitable method(s) and/or portion(s)thereof.

In accordance with at least one aspect of this disclosure, a compositestrip for a composite structure can have at least one transverse endwith a filler edge having a filler edge geometry between a first surfaceand second surface, the second surface being opposite the first surface,the filler edge geometry configured to prevent formation of one or moregaps between one or more adjacent composite strips. The filler edgegeometry can be any suitable filler edge geometry as disclosed herein,e.g., as described above.

In accordance with at least one aspect of this disclosure, a compositestructure can be formed of or can include a plurality of compositestrips. The plurality of composite strips can include one or more fillerstrips which can have at least one lateral filler edge having a filleredge geometry between a first surface and second surface, the secondsurface being opposite the first surface. The lateral filler edgegeometry can be configured to prevent formation of and/or reduce thesize of one or more gaps between one or more adjacent composite strips.The filler edge geometry can be any suitable filler edge geometrydisclosed herein (e.g., as described above, e.g., with respect totransverse end embodiments).

In certain embodiments, the at least one lateral filler edge can be onboth lateral sides of the one or more composite strips. The one or morecomposite structures includes one or more of the composites stripsdisposed on or adjacent to another of the one or more composite strips.One or more of the at least one lateral filler edge can be locatedadjacent to or in overlapping contact with a substantially parallel,neighboring strip.

In certain embodiments, the composite strips can have symmetric lateraledges (e.g., having the same filler edge geometry mirrored). In certainembodiments, the composite strips can have asymmetric lateral edges suchthat adjacent composite strips have complimentary overlapping edges toreduce or eliminate a gap.

In certain embodiments, the structure can include a plurality ofcomposite strips having one or more overlapping lateral edges. Any othersuitable strip placement and/or arrangement to reduce or eliminatefiller gap volume is contemplated herein.

In accordance with at least one aspect of this disclosure, a method caninclude forming at least one lateral edge of the composite strip to havea lateral filler edge having a filler edge geometry between a firstsurface and second surface, the second surface being opposite the firstsurface, the filler edge geometry configured to prevent formation ofand/or reduce a size of one or more gaps between one or more adjacentcomposite strips. The method can also include laying parallel compositestrips having lateral filler edges adjacent to or overlapping each otherto form a composite structure. In certain embodiments, forming caninclude one or more of cutting, and/or clamping or roller clamping theend of the composite strip into a form.

In accordance with at least one aspect of this disclosure, a compositestrip for a composite structure can have at least one lateral filleredge having a filler edge geometry between a first surface and secondsurface, the second surface being opposite the first surface, the filleredge geometry configured to prevent formation of and/or reduce a size ofone or more gaps between one or more adjacent composite strips. Thefiller edge geometry can be any suitable filler edge geometry disclosedherein, e.g., as described above.

These and other features of the embodiments of the subject disclosurewill become more readily apparent to those skilled in the art from thefollowing detailed description taken in conjunction with the drawings.

BRIEF DESCRIPTION OF THE DRAWINGS

So that those skilled in the art to which the subject disclosureappertains will readily understand how to make and use the devices andmethods of the subject disclosure without undue experimentation,embodiments thereof will be described in detail herein below withreference to certain figures, wherein:

FIG. 1A is an embodiment of an Automated Fiber Placement (AFP) system inaccordance with this disclosure, showing a fiber-reinforced strip beinglaid on a mold surface, for example.

FIG. 1B shows a perspective view of an embodiment of a hollow shaftcomposite structure in accordance with the disclosure;

FIG. 1C shows an axial cross-sectional view of the embodiment of FIG.1B; and

FIG. 1D shows a close up the embodiment of FIG. 1C.

FIG. 2 is a perspective view of an end portion of an embodiment of afiber-reinforced strip having a filler edge in accordance with thisdisclosure, showing a non-straight transverse edge (e.g., an axial end)having a chamfer;

FIG. 3 is a perspective view of an end portion of an embodiment of afiber-reinforced strip having a filler edge in accordance with thisdisclosure, showing a non-straight transverse edge having a doublebevel;

FIG. 4 is a perspective view of an end portion of an embodiment of afiber-reinforced strip having a filler edge in accordance with thisdisclosure, showing both non-straight lateral edges having a chamfer;

FIG. 5 is a perspective view of an end portion of an embodiment of afiber-reinforced strip having a filler edge in accordance with thisdisclosure, showing both non-straight lateral edges having a doublebevel;

FIG. 6 is a through-thickness cross-sectional view of an embodiment of afiber-reinforced strip without a filler edge, shown having a straighttransverse edge or lateral edge;

FIGS. 7A, 7B, 7C, 7D, 7E, 7F, 7G, and 7H are through-thicknesscross-sectional views of embodiments of a fiber-reinforced strip havinga filler edge in accordance with this disclosure;

FIGS. 8A and 8B illustrate a portion of laminated composite structureformed using the embodiment with a filler edge of FIG. 6 , where as aresult of sandwiching between neighboring layers, a residual gap isformed as a polymeric pocket;

FIGS. 9A, 9B and 9C illustrate a portion of a laminated compositestructure formed using the embodiment of FIG. 7A having a filler edge,shown advanced filling without or reduced polymeric pocket (FIG. 9B) inwhere the residual gap in FIGS. 8A-8B would be, wherein FIG. 9C shows anembodiment of the composite structure, the bottom layer being straight,e.g., formed on a mold;

FIG. 10 illustrates a portion of a laminated composite structure (e.g.,a tapered segment) formed using the embodiment of FIG. 6 , showingresidual gaps formed;

FIG. 11 illustrates the portion of a laminated composite structuresimilar to that of FIG. 10 , formed using the embodiment of FIG. 7A,showing no gaps formed;

FIG. 12 illustrates a portion of a laminated composite structure formedusing the embodiment of FIG. 6 , wherein two edges of adjacent stripsare shown spaced and showing residual gaps formed as a result;

FIG. 13 illustrates the portion of a laminated composite structuresimilar to that of FIG. 12 , formed using the embodiment of FIG. 7A,showing no gaps formed;

FIG. 14 illustrates a portion of a laminated composite structure formedusing the embodiment of FIG. 6 , wherein two edges of adjacent stripsare shown overlapping, and showing residual gaps formed as a result;

FIG. 15 illustrates the portion of a laminated composite structuresimilar to that of FIG. 14 , formed using the embodiment of FIG. 7A,showing no gaps formed;

FIGS. 16A, 16B, 16C, and 16D illustrate embodiments of laminatedcomposite structures in accordance with this disclosure, shown utilizingthe embodiment of FIG. 6 and having residual gaps (polymeric pockets),wherein FIGS. 16A and 16B illustrate axial an cross-sectional view of atrough thickness, wherein FIG. 16C illustrates axial cross-sectionalview of an axi-symmetric embodiment (e.g., hollow shaft), and whereinFIG. 16D illustrates a perspective view of laminated shell.

FIGS. 17A, 17B, 17C, and 17D illustrate embodiments of compositestructures in accordance with this disclosure, similar to FIGS. 16A-D,respectively, shown utilizing the embodiment of FIG. 7A and having nopolymeric pockets; wherein FIGS. 17A and 17B illustrate an axialcross-sectional view of a trough thickness, wherein FIG. 17C illustratesan axial cross-sectional view of an axi-symmetric embodiment (e.g.,hollow shaft), and wherein FIG. 17D illustrates a perspective view oflaminated shell.

FIG. 18 illustrates an embodiment of a cutting process in accordancewith this disclosure for forming an embodiment, e.g., as shown in FIGS.2, 4, and 7A;

FIGS. 19A and 19B illustrate an embodiment of a cutting process inaccordance with this disclosure for forming an embodiment, e.g., asshown in FIGS. 3, 5, 7B, and 7C;

FIG. 20 illustrates an embodiment of a clamping process in accordancewith this disclosure for forming an embodiment, e.g., as shown in FIGS.2 and 4 ;

FIG. 21 illustrates an embodiment of a clamping process in accordancewith this disclosure for forming an embodiment, e.g., as shown in FIGS.3 and 5 ;

FIG. 22 illustrates an embodiment of a roller clamping process inaccordance with this disclosure for forming an embodiment, e.g., asshown in FIGS. 2 and 4 ;

FIG. 23 illustrates an embodiment of a laser cutting process inaccordance with this disclosure for forming an embodiment, e.g., asshown in FIG. 2 ;

FIG. 24 illustrates an embodiment of a laser cutting process inaccordance with this disclosure for forming an embodiment, e.g., asshown in FIG. 3 ;

FIG. 25 illustrates an embodiment of a laser cutting process inaccordance with this disclosure for forming an embodiment, e.g., asshown in FIG. 4 ;

FIG. 26 illustrates an embodiment of a laser cutting process inaccordance with this disclosure for forming an embodiment, e.g., asshown in FIG. 5 ;

FIG. 27 illustrates an embodiment of a roller clamping process inaccordance with this disclosure for forming an embodiment, e.g., asshown in FIG. 5 ;

FIGS. 28A, 28B, 28C and 28D illustrate certain embodiments of rollerclamp profiles for forming linear, concave, convex, and complex filleredge geometries, respectively; and

FIGS. 29A, 29B, 29C, 29D, and 29E, show certain embodiments of stripshaving lateral filler edge geometry laid up adjacent each other (e.g.,axial/long direction into the page), wherein FIG. 29A shows symmetricshapes, FIG. 29B shows non-symmetric shapes, FIG. 29C showsdouble-curvature profiled shape, FIG. 29D shows symmetric shapes placedin an alternating up/down pattern, and FIG. 29E shows double-curvatureprofiled shape laid in an up/down sequence.

DETAILED DESCRIPTION

Reference will now be made to the drawings wherein like referencenumerals identify similar structural features or aspects of the subjectdisclosure. For purposes of explanation and illustration, and notlimitation, an illustrative view of an embodiment of a system inaccordance with the disclosure is shown in FIG. 1A and is designatedgenerally by reference character 100. Other embodiments and/or aspectsof this disclosure are shown in FIG. 1B-29. Certain embodimentsdescribed herein can be used to make improved composite structures(e.g., for aircraft).

Referring to FIG. 1A, an Automated Fiber Placement (AFP) system 100 caninclude suitable components to form a strip (e.g., a tape havingadhesive and/or resin, such as fiber-reinforced polymer-matrix) using atow. The system 100 can include any suitable components appreciated bythose skilled in the art of AFP, e.g., as schematically shown in FIG.1A. The system 100 can include a cutting device 101 (e.g., a blade orlaser) to cut a transverse end of the strip to form a cut stripseparated from the tow.

The system 100 can additionally include a clamping device 103 to clamp(e.g., a linear clamp or roller clamp) or cut (e.g., by laser) in anysuitable position to shape the edges of the tow when laying strips ofthe tow. The cutting device 101 can also include a clamping deviceassociated therewith to clamp a transverse end of a strip (e.g., aftercutting), for example. The system 100 can be configured to lay strips105 along a mold surface 107 to form a composite structure having ashape of the mold 109. The system 100 can be configured to form and layone or more embodiments of a strip disclosed below for forming alaminated composite structure.

In accordance with at least one aspect of this disclosure, a compositestructure (e.g., structure 150 as shown in FIGS. 1B, 1C, and 1D) can beformed of or can include a plurality of composite continuous strips 151(e.g., formed from a composite fiber-reinforced tow and/or made offibers which can be adhered to a surface, e.g., using epoxy). Theplurality of composite strips 151, 153 can include one or more fillerstrips 153 (e.g., discontinuous strips) of finite shorter length. Anysuitable combination of continuous 151 and discontinuous 153 strips canbe used to create tapered shapes 161 of desired geometries. For example,in certain embodiments, tapered shapes can be beneficial in areas whereincreased thickness may be needed, for example, for rivet- or bolt-basedcomposite/metal joints. The filler strips 153 can have at least onefiller edge 155 having a filler edge geometry between a first surface157 and second surface 159, the second surface 159 being opposite thefirst surface 157. The filler edge geometry can be configured to preventformation of one or more gaps between one or more adjacent compositestrips (e.g., formed by a shorter length strip sandwiched by longerlength strips, or formed by overlap or space between two parallelstrips).

Referring additionally to FIG. 2 , the filler edge geometry of thefiller edge 155 can be non-straight (e.g., a non-flat, non-90 degreeface as shown in FIG. 6 ) between the first surface 157 and the secondsurface 159 of the one or more composite strips 153. For example, thefiller edge geometry can have a chamfer, e.g., as shown in FIG. 1B andFIG. 2 , between the first surface 157 and the second surface 159. Thechamfer can be a straight slope 155 a that connects the first surface157 and the second surface 159, for example. In embodiments, a non-flatfiller edge may not be not entirely accurate of surfaces that includeflat surfaces, such as angles, for example.

In certain embodiments, as shown in FIG. 1B and FIG. 2 , the at leastone filler edge 155 (having a single linear slope 155 a) can be atransverse end (e.g., end of the long axis, or an axial end) of the oneor more composite strips 153. The one or more composite structures 150can include a plurality of layers of strips 151 (and/or strips 153)sandwiching at through thickness of the transverse end, e.g., as shown.The transverse end (where filler edge 153 is) can be located at atransition position 161 (e.g. a tapered region) where there is a changein a total amount of layers, which can result in a change in the totalamount of through thickness for the composite strips 151, 153. Forexample, as shown, the structure 150 has an end with more layers ofstrips 151, 153 that tapers down to a thinner section with less layersof strips 151. As a result, strips 153 are shorter than strips 151 andterminate within the layer structure. In certain embodiments, anysuitable angle or orientations (e.g., including crossing a filler underan angle different than 90 degrees) can be used as well whilemaintaining a “transverse” end as described herein.

Certain other embodiments of strips and filler edges are shown in FIGS.3, 4, and 5 , for example. For example, in FIG. 3 , in certainembodiments, the strip 353 can have a filler edge 355 with filler edgegeometry that can be a double beveled shape having a first straightslope 355 a from the first surface 157 to a tip 355 b, and a secondstraight slope 355 c from the second surface 159 to the tip 355 b. FIG.4 shows an embodiment of a strip 453 having lateral filler edges 455 onboth lateral sides with filler edge geometry similar to that of FIG. 2having a chamfer with a single straight slope 455 a. FIG. 5 shows anembodiment of a strip 553 having lateral filler edges 555 on bothlateral sides similar to that of FIG. 3 having a double bevel shape.

For comparison, FIG. 6 shows a straight end without a filler geometry,which may be typically used in conventional AFP manufacturing processes.The straight end has an approximately 90 degree straight face betweenthe first surface and the second surface. As defined herein, the term“non-straight” end does not include the embodiment shown in FIG. 6 . Theembodiment of FIG. 6 includes a rectangular cross-sectional shape.

Referring to FIGS. 7A-7H, various filler edge geometries are shown. FIG.7A shows a cross-section having a single straight slope with a singleangle (alpha), e.g., similar to that of FIG. 2 . FIG. 7B shows a doublebevel having two straight slopes with two angles (alpha 1 and alpha 2)which can be the same or different.

In certain embodiments, as shown in FIG. 7C, the first straight slopeand the second straight slope can have different lengths and/or slopes.For example, the length of the bottom bevel is longer than that of thetop bevel, and the two angles (alpha 1 and alpha 2) can be the same ordifferent.

As shown in FIGS. 7D-7H, the filler edge geometry can include a curvedshape having at least a first curved slope from the first surface to atip (e.g., as shown in FIGS. 7F-7H) and/or the second surface (e.g., asshown in FIGS. 7D and 7E). In certain embodiments, the first curvedslope can be convex (e.g., as shown in FIGS. 7D and 7F). In certainembodiments, the first curved slope can be concave (e.g., as shown inFIGS. 7E and 7G).

In certain embodiments, the curved shape can include a second curvedslope between the second surface and the tip (e.g., as shown in FIGS.7F-7H). The first curved slope and/or the second curved slope can beconvex or concave, or a combination thereof (e.g., the first curvedslope and the second curved slope can be the same or different). Incertain embodiments, the curved shape can be a complex shape, e.g., asshown in FIG. 7H, having complex curved surfaces with varying slope. Incertain embodiments, curvatures of the first and/or the second curvedslopes can be defined by either uniform or non-uniform radii. Anysuitable combinations of the above noted linear and curved segments canbe applied when needed to achieve the desired properties.

Various embodiments and their applications are described below incomparison to the straight end of FIG. 6 . For example, FIGS. 8A and 8Billustrate a composite laminated structure formed using the embodimentwithout a filler edge, i.e., as illustrated in FIG. 6 , showing aresidual gap before (e.g., FIG. 8A) and after (e.g., FIG. 8B) forming.Here, embodiments can be formed with finite-length fiber-reinforcedlayers or strips. FIGS. 9A, 9B and 9C illustrate a composite laminatedstructure formed using the embodiment of FIG. 7A having a filler edge,shown filling in where the residual gap in FIGS. 8A-8B would be. FIG. 9Cshows the bottom layer being straight, e.g., formed on a mold.

FIG. 10 illustrates a portion of a laminated composite structure (e.g.,a tapered segment at connection end of a hollow shaft) formed using theembodiment of FIG. 6 , showing residual gaps formed. FIG. 11 illustratesthe portion of a composite structure similar to that of FIG. 10 , formedusing the embodiment of FIG. 7A, showing no gaps formed.

FIG. 12 illustrates a portion of a laminated composite structure formedusing the embodiment of FIG. 6 , such that two edges (e.g., lateralsides) of adjacent strips are shown spaced and showing residual gapsformed as a result. The gap can be any suitable gap, whether empty spaceor filled with a material. For example, in embodiments, the gaps can befilled with polymer matrix, where there no “empty” space. In this, thegaps can be filled polymer matrix without reinforcement (i.e., fibers).Accordingly, as used herein, “gap” means an area without reinforcingfibers.” FIG. 13 illustrates the portion of a composite structuresimilar to that of FIG. 12 , formed using the embodiment of FIG. 7A,showing no gaps formed.

FIG. 14 illustrates a portion of a laminated composite structure formedusing the embodiment of FIG. 6 , wherein two edges of adjacent stripsare shown overlapping, and showing residual gaps formed as a result.FIG. 15 illustrates the portion of a composite structure similar to thatof FIG. 14 , formed using the embodiment of FIG. 7A, showing no gapsformed.

FIGS. 16A, 16B, 16C, and 16D illustrate embodiments of compositestructures in accordance with this disclosure, shown utilizing theembodiment of FIG. 6 and having resin pockets. FIGS. 17A, 17B, 17C, and17D illustrate embodiments of composite structures in accordance withthis disclosure, similar to FIGS. 16A-D, respectively, shown utilizingthe embodiment of FIG. 7A and having no resin pockets.

Referring additionally to FIGS. 16A-17D, in certain embodiments, thecomposite structure 1700A, 1700B can form a linear (e.g., FIG. 17A) orcurved (e.g., FIG. 17B) laminated beam, respectively. The compositestructure 1700C can form a hollow laminated component (e.g. acylindrical shaft or beam), e.g., axi-symmteric or non-axi-symmterictubes (FIG. 17C). Similarly, the composite structure 1700D can form alaminated curved shell of flat plate with tapered regions in one or twodirections (e.g. as shown in FIG. 17D). Such embodiments can havechanging layer amounts at one or more ends thereof such that the one ormore ends have more total layers. In certain embodiments, e.g., as shownin FIGS. 1D, 17A-17D, the one or more composite strips 153 can formterminal layers at the one or more ends of the structure (e.g., as shownin FIGS. 1B-1D, 17A, 17B, 17C, and 17D) that do not extend the entirelength (in at least one axis). As shown in FIGS. 17A-17D, the filleredges can be located where one or more longer layers 151 bend (e.g.,where a polymeric and/or resin gap would have existed otherwise).

In certain embodiments, the composite strips can form a curvedstructure, e.g., as shown in FIG. 17B (shown curved in a singledimension) and FIG. 17D (curved in multiple dimensions). The filleredges can be located where one or more longer layers 151 bend, similarto that of FIGS. 17A and 17C. Any other suitable composite structureshapes, layer arrangements, and/or purpose are contemplated herein.

In accordance with at least one aspect of this disclosure, a method caninclude laying a composite strip to form a composite structure, andcutting or otherwise forming at least one transverse end of thecomposite strip to have a filler edge having a filler edge geometrybetween a first surface and second surface, the second surface beingopposite the first surface, the filler edge geometry configured toprevent formation of one or more gaps between one or more adjacentcomposite strips. In certain embodiments, cutting or otherwise formingcan include cutting the end of the composite strip at a non-90 degreeangle, e.g., as shown in FIGS. 18 and 19A-19B.

Cutting the end can include making a single cut to form a chamfer (e.g.,as shown in FIG. 18 ), or a double cut to form a double bevel with a tip(e.g., as shown in FIGS. 19A and 19B). Cutting or otherwise forming caninclude clamping the end of the composite strip into a form (e.g., asshown in FIGS. 20, 21, and 22 ). Clamping can include single angleclamping (e.g., as shown in FIG. 20 ), or double angle clamping (e.g.,as shown in FIG. 21 ). Any suitable type of cutting (e.g., with a blade,with a laser), and/or clamping, e.g., compression clamping (e.g., shownin FIGS. 20 and 21 ) or roller clamping (e.g., as in FIG. 22 ) iscontemplated herein. The method can include any other suitable method(s)and/or portion(s) thereof.

FIG. 23 illustrates an embodiment of a laser cutting process inaccordance with this disclosure for forming an embodiment, e.g., asshown in FIG. 2 . As shown, the system 100 can include a single lasercutter 101 that can be positioned to cut a transverse end of the stripat a single angle.

FIG. 24 illustrates an embodiment of a laser cutting process inaccordance with this disclosure for forming an embodiment, e.g., asshown in FIG. 3 . As shown, the system 100 can include two laser cutters101 that can be positioned to cut a transverse end of the strip at twoangles (the same or different) to form a double bevel.

FIG. 25 illustrates an embodiment of a laser cutting process inaccordance with this disclosure for forming an embodiment, e.g., asshown in FIG. 4 . As shown, the system 100 can include two laser cutters103 that can be positioned to cut each lateral edge of the strip at asingle angle to form a chamfer on each lateral side.

FIG. 26 illustrates an embodiment of a laser cutting process inaccordance with this disclosure for forming an embodiment, e.g., asshown in FIG. 5 . As shown, the system 100 can include four lasercutters 103 that can be positioned to cut a transverse end of the stripat two angles to form a double bevel on each lateral side.

FIG. 27 illustrates an embodiment of a roller clamping process inaccordance with this disclosure for forming an embodiment, e.g., asshown in FIG. 5 , e.g., to form a double bevel.

FIGS. 28A, 28B, 28C, 28D illustrate certain embodiments of roller clampprofiles for forming linear, concave, convex, and complex (e.g. adouble-curvature) filler edge geometries, respectively. Any suitableshapes to form any suitable filler edge is contemplated herein.

In certain embodiments, top and bottom rollers can have the same ordifferent profiles. In certain embodiments, left and right lateral setsof rollers can be symmetric or anti-symmetric.

While certain filler edge geometries are shown and described above, andsuitable shape to fill in a gap (e.g., a resin pocket) formed in acomposite structure is contemplated herein. While embodiments havingtransverse end filler edges and lateral filler edges are shown, andsuitable lateral and/or transverse ends can have filler edges,separately or together. For example, a single lateral filler edge and asingle transverse filler edge can be combined. In certain embodiments,all edges and ends can be filler edges. Any combination of embodimentsis contemplated herein.

In accordance with at least one aspect of this disclosure, a compositestrip (e.g., filler strips 153 or 453 as shown in FIGS. 2 and 4 ) for acomposite structure (e.g., structure 150) can have at least onetransverse end (e.g., one or both cut ends) with a filler edge (e.g., asdescribed above) having a filler edge geometry between a first surfaceand second surface, the second surface being opposite the first surface,the filler edge geometry configured to prevent formation of one or moregaps between one or more adjacent composite strips. The filler edgegeometry can be any suitable filler edge geometry as disclosed herein,e.g., as described above.

Referring to FIGS. 29A-29E, in accordance with at least one aspect ofthis disclosure, a composite structure can be formed of or can include aplurality of composite strips. The plurality of composite strips caninclude one or more filler strips (e.g., strips 353 and 553 as shown inFIGS. 3 and 5 ) which can have at least one lateral filler edge having afiller edge geometry between a first surface and second surface, thesecond surface being opposite the first surface. The lateral filler edgegeometry can be configured to prevent formation of and/or reduce thesize of one or more gaps between one or more adjacent composite strips.The filler edge geometry can be any suitable filler edge geometrydisclosed herein (e.g., as described above, e.g., with respect totransverse end embodiments).

FIGS. 29A, 29B, 29C, 29D, and 29E show certain embodiments of stripshaving lateral filler edge geometry laid up adjacent each other (e.g.,axial/long direction into the page). FIG. 29A shows an embodiment havingflat edges. a. FIGS. 29B and 29C show non-symmetric shapes, and FIGS.29D and 29E show symmetric shapes places in an alternating up/downpattern. In certain embodiments, the strips can have nestingconcave/convex shapes or alternating convex and concave filler edgegeometry strips that mate with each other. FIGS. 29B and 29D show linearslope edges. FIGS. 29C and 29E show non-linear curved slope edges. FIG.29D shows a trapezoidal shape laid in an up/down sequence (e.g., two AFParms can be used in parallel). FIG. 29E shows double-curvature profiledshape laid in an up/down sequence (e.g., two AFP arms can be used inparallel). In embodiments, the convex/concave edges can be curved ordouble-slope shapes, and the convex/convex with concave/concave sequencecan have two AFP arms used in parallel.

In certain embodiments, the at least one lateral filler edge can be onboth lateral sides of the one or more composite strips (e.g., as shownin FIGS. 4 and 5 ). As shown in FIGS. 13 and 15 , the one or morecomposite structures includes one or more of the composites stripsdisposed on or adjacent to another of the one or more composite strips.Each lateral filler edge can be located adjacent to (e.g., as shown inFIG. 13 ) or in overlapping contact with (e.g., as shown in FIG. 15 ) asubstantially parallel strip.

In certain embodiments, the composite strips can have symmetric lateraledges (e.g., having the same filler edge geometry mirrored), e.g., asshown in FIGS. 29D-29E. In certain embodiments, the composite strips canhave asymmetric lateral edges such that adjacent composite strips havecomplimentary overlapping edges to reduce or eliminate a gap, e.g., asshown in FIGS. 29B and 29C.

In certain embodiments, the structure can include a plurality ofcomposite strips having one or more overlapping lateral edges (e.g., asshown in FIGS. 15 and 29B-29E). Any other suitable strip placementand/or arrangement to reduce or eliminate filler gap volume iscontemplated herein.

In accordance with at least one aspect of this disclosure, a method caninclude forming at least one lateral edge of the composite strip to havea lateral filler edge having a filler edge geometry between a firstsurface and second surface, the second surface being opposite the firstsurface, the filler edge geometry configured to prevent formation ofand/or reduce a size of one or more gaps between one or more adjacentcomposite strips. The method can also include laying parallel compositestrips having lateral filler edges adjacent to or overlapping each otherto form a composite structure (e.g., as shown in FIGS. 13, 15, and29B-29E). In certain embodiments, forming can include clamping or rollerclamping the end of the composite strip into a form.

In accordance with at least one aspect of this disclosure, a compositestrip for a composite structure can have at least one lateral filleredge having a filler edge geometry between a first surface and secondsurface, the second surface being opposite the first surface, the filleredge geometry configured to prevent formation of and/or reduce a size ofone or more gaps between one or more adjacent composite strips. Thefiller edge geometry can be any suitable filler edge geometry disclosedherein, e.g., as described above.

Embodiments include a method of making composite drive shafts withenhanced damage tolerance. Embodiments can use Automated Fiber Placement(AFP). Embodiments can be applicable to any suitable compositestructure. Embodiments can allow for a reduction of damage risk incomposite drive shafts with non-uniform thickness, e.g., made with AFPmanufacturing processes. During the AFP manufacturing process,embodiments can be constructed by placing fiber-reinforced compositelayers on molds or mandrels in an automated fashion using a number ofseparate small width strips of thermoset or thermoplastic preimpregnatedmaterials to form composite layups. In embodiments, other compositemanufacturing methods may be used to create fiber-reinforcedpolymer-matrix composite strips or layers with finite width or/andlength.

Embodiments of a method lay strips like a tape. Short ply layers havefinite length and cause formation of resin pockets due to straight endtermination. These resin filled pockets are weaker than fiber and createweakness points, and lower damage tolerance in both initiation anddamage growth. Embodiments can use a strip/tape made up of a tow ofcarbon fiber, glass fiber, organic fiber, or any other suitable fiber,as well as polymers such as thermosets and thermoplastics. Embodimentscan include a non-sharp transversal edge with a double slope, anon-sharp transversal edge with a single slope, non-sharp longitudinaledge with a double slope on each side of the tape, and/or a non-sharplongitudinal edge with a single slope on each side of the tape.

Embodiments of strips and be formed during layup. Embodiments can be cutin one direction, cut in two directions (e.g., in a two-step process),formed by clamping from one side, formed by clamping from both sides,formed by “roller” clamps from one or both sides, and/or formed byclamping and then cutting of remaining “squeezed” part.

Embodiments can be utilized to make drive shafts (DS) made of advancedfiber-reinforced polymer-matrix composite materials. While compositematerials do provide significant weight reduction, there are significantchallenges associated with their structural integrity, namely in areasof non-uniform thickness. Such areas are used typically in zones of a)joints (extra thickness to compensate stress concentration due tofasteners), b) rub-rings (extra thickness to mitigate potentialcontacts), or c) belts for reinforcement in the circumferentialdirections for buckling resistance enhancement.

Drive shafts may exhibit through-thickness gaps between neighboringplies in such zones, where the gaps can be filled by the polymer matrix.Since stiffness of the polymer is much lower than stiffness offiber-reinforced plies, there may be additional stress concentrationsunder applied load in such zones. Although such gaps can be eventuallyfilled with the polymer matrix, there are no reinforced fibers insidethe gaps and, therefore, they are typical locations of stressconcentrations due to differences in stiffness between fiber-reinforcedstrips and non-reinforced gaps. Due to these stress concentrations, thegaps are among the most probable locations for damage initiation andgrowth.

Additional thickness is implemented by short plies with finite lengthgenerating considerable resin pockets at their ends. Such resin pocketscan be seen on actual micrographs. These resin pockets are prime sourcesof damage initiation and follow-up damage growth for a typical damagepattern. Resin pockets are the most dangerous for damages due to stressconcentrations in their areas because of big differences in stiffness ofthe resin itself and fiber-reinforced plies. Thus, embodiments allowenhanced damage tolerance in composite DS and other structures to causea reduction of damage initiation risks.

Certain structures can be made with AFP, allowing an efficient way ofmaking shafts with non-uniform thickness (among other benefits of AFP).The Conventional AFP implementations result in narrow plies, havingrectangular shapes with sharp straight edges (e.g., as shown in FIG. 6). In other words, conventional AFP also has the same problem with resinpockets and high risk of damage initiation in these areas.

Embodiments includes designs and methods of making such designs. Incontrast with a conventional design with sharp “rectangular” shapes ofindividual AFP-generated plies (e.g., as shown in FIG. 6 ), embodimentsinclude non-sharp edges (e.g., FIG. 2 - FIG. 5 ). Designs shown in FIGS.2 and 3 illustrate shape modification for a transversal edge, and FIGS.4 and 5 for lateral/longitudinal edges, for example. There can becombinations of both locations for shape modifications, i.e., at bothtransversal and longitudinal edges. In addition, there can bemodifications by two slopes (e.g., FIGS. 3 and 5 ) or with one slope(e.g., FIGS. 2 and 4 ).

Such non-sharp edges can provide a significant difference in post-curingor post-consolidation implementations. Embodiments of structures usingembodiments of strips may have little or no resin pockets, while theconventional methods still have a large concentration of resin (polymer)as a source of damages due to considerable stress concentration. Similaradvantage verse the conventional design is illustrated at FIGS. 10-15for zones with monotonic increased thickness (FIGS. 10 and 11 ), reducedthickness (FIGS. 12 and 13 ) and local thickness increase (FIGS. 14 and15 ). More advanced shapes of non-sharp edges are listed, among others,in FIGS. 7A-7H (which are applicable to both transversal andlongitudinal/lateral edges).

Embodiments can be applied to a broad range of composite structures,such as tapered straight (or almost straight) components (e.g., FIG.16A), tapered curved components (e.g., FIG. 16B), tapered hollowcomponents (with open or closed cross-section), e.g., drive shaftsthemselves or other tubular designs (e.g., FIG. 16C), anddouble-curvature (double-tapered) components (e.g., FIG. 16D).

Embodiments of methods can include cutting of ply edges before or duringlayup by AFP. FIGS. 18-19B illustrate potential implementations bycutting of ply edges according to desired shapes. FIGS. 20-21 show amanufacturing method by clamping of edges for desired shape, and FIG. 22illustrates a roller clamping method. Embodiments can utilize combinedclamping and cutting, for example, by cutting of excessive materialafter clamping.

Embodiments are applicable to both thermoplastics (TP) and thermoset(TS) polymeric matrices in considered fiber-reinforced composites, forexample. In the case of TP implementation, polymer consolidation may beused in the post-layup stage, while for TS, curing may be used. Withrespect to reinforced fibers, carbon, glass, organic and otherhigh-strength fibers known in the field may be used.

Embodiments can enable mass production of complex composite structuresusing AFP, for example. Embodiments can provide improved damagetolerance through reduced risks of either damage initiation or growth orboth. Embodiments can provide improved damage tolerance for pristinecomposite DS and also, during service, e.g., with potential impactdamages. Improved damage tolerance is associated with longer service,reduced maintenance/inspection cost, reduced weight, and reinforcementof reputation in field of composite aircraft drive systems.

Those having ordinary skill in the art understand that any numericalvalues disclosed herein can be exact values or can be values within arange. Further, any terms of approximation (e.g., “about”,“approximately”, “around”) used in this disclosure can mean the statedvalue within a range. For example, in certain embodiments, the range canbe within (plus or minus) 20%, or within 10%, or within 5%, or within2%, or within any other suitable percentage or number as appreciated bythose having ordinary skill in the art (e.g., for known tolerance limitsor error ranges).

The articles “a”, “an”, and “the” as used herein and in the appendedclaims are used herein to refer to one or to more than one (i.e., to atleast one) of the grammatical object of the article unless the contextclearly indicates otherwise. By way of example, “an element” means oneelement or more than one element.

The phrase “and/or,” as used herein in the specification and in theclaims, should be understood to mean “either or both” of the elements soconjoined, i.e., elements that are conjunctively present in some casesand disjunctively present in other cases. Multiple elements listed with“and/or” should be construed in the same fashion, i.e., “one or more” ofthe elements so conjoined. Other elements may optionally be presentother than the elements specifically identified by the “and/or” clause,whether related or unrelated to those elements specifically identified.Thus, as a non-limiting example, a reference to “A and/or B”, when usedin conjunction with open-ended language such as “comprising” can refer,in one embodiment, to A only (optionally including elements other thanB); in another embodiment, to B only (optionally including elementsother than A); in yet another embodiment, to both A and B (optionallyincluding other elements); etc.

As used herein in the specification and in the claims, “or” should beunderstood to have the same meaning as “and/or” as defined above. Forexample, when separating items in a list, “or” or “and/or” shall beinterpreted as being inclusive, i.e., the inclusion of at least one, butalso including more than one, of a number or list of elements, and,optionally, additional unlisted items. Only terms clearly indicated tothe contrary, such as “only one of or “exactly one of,” or, when used inthe claims, “consisting of,” will refer to the inclusion of exactly oneelement of a number or list of elements. In general, the term “or” asused herein shall only be interpreted as indicating exclusivealternatives (i.e., “one or the other but not both”) when preceded byterms of exclusivity, such as “either,” “one of,” “only one of,” or“exactly one of.”

Any suitable combination(s) of any disclosed embodiments and/or anysuitable portion(s) thereof are contemplated herein as appreciated bythose having ordinary skill in the art in view of this disclosure.

The embodiments of the present disclosure, as described above and shownin the drawings, provide for improvement in the art to which theypertain. While the subject disclosure includes reference to certainembodiments, those skilled in the art will readily appreciate thatchanges and/or modifications may be made thereto without departing fromthe spirit and scope of the subject disclosure.

What is claimed is:
 1. A composite structure formed of or including aplurality of composite strips, wherein the plurality of composite stripsinclude one or more filler strips which have at least one filler edgehaving a filler edge geometry between a first surface and secondsurface, the second surface being opposite the first surface, the filleredge geometry configured to prevent formation of one or more gapsbetween one or more adjacent composite strips.
 2. The compositestructure of claim 1, wherein the filler edge geometry is non-straightbetween the first surface and the second surface of the one or morecomposite strips.
 3. The composite structure of claim 2, wherein thefiller edge geometry has a chamfer between the first surface and thesecond surface.
 4. The composite structure of claim 1, wherein the atleast one filler edge is a transverse end of the one or more compositestrips, wherein the one or more composite strips includes a plurality oflayers sandwiching the transverse end.
 5. The composite structure ofclaim 4, wherein the transverse end is located at a transition positionwhere there is a change in a total amount of layers.
 6. The compositestructure of claim 4, wherein the filler edge geometry is a doublebeveled shape having a first straight slope from the first surface to atip, and a second straight slope from the second surface to the tip. 7.The composite structure of claim 6, wherein the first straight slope andthe second straight slope have different lengths and/or slopes.
 8. Thecomposite structure of claim 4, wherein the filler edge geometryincludes a curved shape having at least a first curved slope from thefirst surface to a tip and/or the second surface.
 9. The compositestructure of claim 8, wherein the first curved slope is convex.
 10. Thecomposite structure of claim 8, wherein the first curved slope isconcave.
 11. The composite structure of claim 8, and wherein the curvedshape includes a second curved slope from the second surface to the tip.12. The composite structure of claim 1, wherein the one or more fillerstrips include fiber-reinforced polymer-matrix filler strips.
 13. Thecomposite structure of claim 1, wherein the composite structure forms alaminated solid beam or hollow laminated beam having changing layeramounts along a beam length at one or more ends thereof such that theone or more ends have more total layers, wherein the one or morecomposite strips form terminal layers at the one or more ends that donot extend the entire length, wherein the filler edges are located atthe one or more ends of the terminal layers.
 14. The composite structureof claim 13, wherein the composite strips forms a curved structure,wherein the filler edges are located at the one or more ends of theterminal layers.
 15. A method, comprising: laying a composite strip toform a composite structure; and cutting or otherwise forming at leastone transverse end of the composite strip to have a filler edge having afiller edge geometry between a first surface and second surface, thesecond surface being opposite the first surface, the filler edgegeometry configured to prevent formation of one or more gaps between oneor more adjacent composite strips.
 16. The method of claim 15, whereincutting or otherwise forming at least one transverse end of thecomposite strip includes cutting the end of the composite strip at anon-90 degree angle with respect to a reinforced fiber orientation. 17.The method of claim 16, wherein cutting the end includes making a singlecut to form a chamfer, or a double cut to form a double bevel with atip.
 18. The method of claim 15, wherein cutting or otherwise formingincludes clamping the end of the composite strip into a form.
 19. Acomposite strip for a composite structure, having at least onetransverse end with a filler edge having a filler edge geometry betweena first surface and second surface, the second surface being oppositethe first surface, the filler edge geometry configured to preventformation of one or more gaps between one or more adjacent compositestrips.
 20. The composite strip of claim 19, wherein the filler edgegeometry has a chamfer between the first surface and the second surface.